How do you calculate the altitude and velocity of a satellite in a geosynchronous orbit of Mars?
1 Answer
The satellite in Mars geostationary orbit must be
Explanation:
To calculate the necessary altitude and velocity needed for a geosynchronous orbit of any planet, you must use a few relationships.
You need to know that the centripetal force exerted on an object in circular motion is
Additionally, you must know that the force of gravitational attraction between any two objects is
Note:
For an object to be in a stable orbit at any altitude, the centripetal force and the gravitational force must be equal. So the first step in solving this problem is to set these expressions equal to each other.
Some simplifying yields
This is the standard form of the equation. If you looked up orbital velocity equation on google, this is what you'd get.
So this equation is fine for a general orbit, but we are trying to find requirements for a geosynchronous orbit. Another relationship is needed.
Luckily, in this type of orbit, since you stay above the same spot on the ground the entire time, you could relate the angular velocities of the planet and the satellite somehow. What people realized is that in a geosynchronous orbit, the period (seconds/cycle) of rotation for the satellite is the same as the planet.
To relate period,
Since velocity,
Simplifying
The mass and rotational period for Mars are known, so you can just plug in the numbers to find the distance from the center of Mars at which you should orbit to become geosynchronous.
or
NOTE: This distance is not altitude! This is the distance from the center of Mars! To find altitude, subtract the radius of Mars from this number. Remember to always use the distance from the core of the planet in these calculations!
or
So now you have your necessary distance. You still don't know how fast it needs to go, but this is an easy step. Just plug it back into the old velocity equation
to get
or
The satellite in Mars geostationary orbit must be stationed